View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66626U 26145.37417948 +.00000000 +00000-0 +70977-3 0 00003
2 66626 53.1596 144.0132 0001779 73.6550 286.4646 15.30189797 08
| Epoch (UTC): | 25 May 2026 08:58:49 |
| Eccentricity: | 0.0001779 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.0132° |
| argument of perigee: | 73.6550° |
| revolutions per day: | 15.30189797 |
| mean anomaly at epoch: | 286.4646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|